| タイトル | Temperature Oscillation in a Loop Heat Pipe with Gravity Assist |
| 本文（外部サイト） | http://hdl.handle.net/2060/20140005700 |
| 著者（英） | Patel, Deepak; Ottenstein, Laura; Robinson, Frank; Ku, Jentung; Garrison, Matt |
| 著者所属（英） | NASA Goddard Space Flight Center |
| 発行日 | 2014-03-25 |
| 言語 | eng |
| 内容記述 | ATLAS Laser Thermal Control System (LTCS) thermal vacuum testing where the condenser-radiator was placed in a vertical position, it was found that the loop heat pipe (LHP) reservoir required much more control heater power than the analytical model had predicted. The required control heater power was also higher than the liquid subcooling entering the reservoir using the measured temperatures and the calculated mass flow rate based on steady state LHP operation. This presentation describes the investigation of the LHP behaviors under a gravity assist mode with a very cold radiator sink temperature and a large thermal mass attached to the evaporator. It is concluded that gravity caused the cold liquid to drop from the condenser-radiator to the reservoir, resulting in a rapid decrease of the reservoir temperature. When the reservoir temperature was increasing, a reverse flow occurred in the liquid line, carrying warm liquid to the condenser-radiator. Both events consumed the reservoir control heater power. The fall and rise of the reservoir temperature also caused the net heat input to the evaporator to vary due to the release and storage of the sensible heat of the thermal mass. The combination of these effects led to a persistent reservoir temperature oscillation and a repeated influx of cold liquid from the condenser. This was the root cause of the extraordinary high control heater power requirement in the LTCS TV test. Without gravity assist, such a persistent temperature oscillation will not be present. |
| NASA分類 | Fluid Mechanics and Thermodynamics |
| レポートNO | GSFC-E-DAA-TN13402 |
| 権利 | No Copyright |
|
